A two phase program was conducted to define requirements and to prepare a preliminary design of a test motor system that will accurately and economically simulate the chamber environments of present and future large solid propellant rocket motors. A segmented motor configuration with 28-in. outside diameter case bonded propellant grains was selected. The nominal grain configuration is an internal burning cylinder with both ends burning.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Ballistic Missile Propellant Evaluation Test Motor System (Super BATES)


    Beteiligte:
    W. A. Stephen (Autor:in) / T. C. Warren (Autor:in) / J. M. Humphrey (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    219 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Ballistic Missile

    W. A. Mrazek | NTIS | 1966


    Missile guidance system against a ballistic missile

    BABA, YORIAKI / TAKANO, HIROYUKI / TAKAO, KICHIRO | AIAA | 1991